Bell 204/205 vs Enstrom F-28

1956–1980s^[source]

1965-present^[source]

1959^[source]

1965^[source]

22 October 1956^[source]

Bell UH-1 Iroquois^[source]

Bell 212 Bell 214^[source]

Enstrom TH180 Spitfire Mark I^[source]

8-9 passengers / 3,000 lb (1,361 kg) equivalent cargo^[source]

two passengers^[source]

1,808 sq ft (168.0 m 2 )^[source]

804 sq ft (74.7 m 2 ) NACA 0013.5^[source]

civilian versions of the UH-1 Iroquois single-engine military helicopter of the Huey family of helicopters^[source]

Bell designed its Model 204 in response to a 1955 United States Army requirement for a utility helicopter. The 204 was a giant step forward in helicopter design, being one of the first to be powered by a turboshaft . The turboshaft engine radically improved the practicality of the helicopter due to its light weight and high power-to-weight ratio , lower fuel consumption, and lower maintenance and operating costs. The use of a turboshaft in the 204 allowed it to carry a useful payload over respectable ranges and at reasonable speeds, which resulted in the 204 and subsequent 205 becoming the most successful western helicopter series in terms of numbers built.^[source]Bell 204/205 · Development; only the objects and conditions stated in this passage

The civil 204B was first delivered in 1961. The subsequent Model 205A-1 is equivalent to the UH-1H, which, compared to the 204, is longer, larger, and has better performance and a more powerful engine.^[source]Bell 204/205 · Development; only the objects and conditions stated in this passage

Fuji-Bell 204B/204B-2 – Civil utility transport helicopter. Built under licence in Japan by Fuji Heavy Industries alongside military HU-1B and HU-1H for the Japan Ground Self Defense Force .^[source]Bell 204/205 · Variants / Bell 204; only the objects and conditions stated in this passage

Bell Helicopter's company designation of the UH-1H.^[source]Bell 204/205 · Variants / Bell 205; only the objects and conditions stated in this passage

Bell 205A – Civil or military utility transport helicopter. Powered by one T53-L-11A, max weight 8,500 pounds, max passenger, 14. Agusta-Bell 205 – Civil or military utility transport helicopter. Built under licence in Italy by Agusta.^[source]Bell 204/205 · Variants / Bell 205; only the objects and conditions stated in this passage

Bell 205A-1 – Civil or military utility transport helicopter version, initial version based on the UH-1H. Powered by one T53-L-13A, max weight 9,500 pounds (10,500 for external loads), max passengers, 14. Agusta-Bell 205A-1 – Modified version of the AB 205.^[source]Bell 204/205 · Variants / Bell 205; only the objects and conditions stated in this passage

Fuji-Bell 205B – a joint Bell-Fuji commercial variant based on UH-1J , a Japanese improved model of UH-1H.^[source]Bell 204/205 · Variants / Bell 205; only the objects and conditions stated in this passage

Bell 210 – Bell Helicopter's designation for a UH-1H, remanufactured and sold as a new aircraft. Powered by one T53-L-17B, same weight capacities as the 205B.^[source]Bell 204/205 · Variants / Bell 205; only the objects and conditions stated in this passage

Global Eagle – Pratt & Whitney Canada name for a modified UH-1H with a new PT6C-67D engine, modified tail rotor, and other minor changes reported to increase range and fuel efficiency over the Bell 212.^[source]Bell 204/205 · Variants / Upgrades; only the objects and conditions stated in this passage

Bell 211 – The HueyTug , was a commercial version of the UH-1C with an upgraded transmission, longer main rotor, larger tailboom, strengthened fuselage, stability augmentation system, and a 2,650 shp (1,976 kW) T55 -L-7 turboshaft engine.^[source]Bell 204/205 · Variants / Derivatives; only the objects and conditions stated in this passage

Capacity: 8-9 passengers / 3,000 lb (1,361 kg) equivalent cargo^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Length: 41 ft 8 in (12.70 m)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Height: 14 ft 7 in (4.45 m)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Empty weight: 4,600 lb (2,087 kg)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Max takeoff weight: 9,500 lb (4,309 kg)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Powerplant: 1 × Lycoming T53-L-11A turboshaft engine, 1,100 shp (820 kW)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Main rotor diameter: 48 ft (15 m)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Main rotor area: 1,808 sq ft (168.0 m 2 )^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Maximum speed: 120 kn (140 mph, 220 km/h)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Cruise speed: 111 kn (128 mph, 206 km/h)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Range: 300 nmi (350 mi, 560 km)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Service ceiling: 19,390 ft (5,910 m)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Rate of climb: 1,755 ft/min (8.92 m/s)^[source]Bell 204/205 · Specifications (204B); only the objects and conditions stated in this passage

Enstrom 480^[source]

Vereinigte Staaten^[source]Country of design · Entwurfsland